Mobil Jet Oil CI
Synthetic aircraft gas turbine oil with added corrosion protection, MIL-PRF-23699 CI
MIL (US) MIL-PRF-23699-CI
Mobil Jet Oil II is a high-performance aircraft-type gas turbine lubricant formulated from a highly stable synthetic base fluid and a unique chemical additive package, giving outstanding thermal and oxidative stability that resists deterioration and deposit formation in both liquid and vapour phases, together with excellent foam resistance. Its effective operating range is -40°C to 204°C, and its high specific heat ensures good heat transfer from oil-cooled engine parts. Extensive laboratory and in-flight testing shows excellent bulk oil stability at temperatures up to 204°C with low evaporation loss. Key benefits include excellent wear and corrosion protection that extends gear and bearing life, retention of viscosity and film strength across a wide temperature range, chemical stability that lowers oil consumption, and a low pour point that eases cold-weather starting. Mobil Jet Oil II is recommended for turbo-jet, turbo-fan, turbo-prop and turbo-shaft (helicopter) gas turbine engines in commercial and military service, as well as industrial and marine applications. It is approved against the Standard Performance (STD) classification of MIL-PRF-23699, is compatible with other synthetic gas turbine lubricants meeting the same specification and with all metals and common seal materials used in gas turbine construction, and carries builder approvals from Honeywell/Lycoming, Rolls-Royce/Allison, CFM International, General Electric, Pratt & Whitney, SNECMA, Turbomeca, Hamilton Sundstrand and others.
| Property | Typical value | Method |
|---|---|---|
| Autogenous-ignition Temperature Test, deg.C, 30 CFR 35.20 | 404 | |
| change in Kinematic viscosity, 72 h @ -40 C% | 0.15 | ASTM D2532 |
| Density @ 15 Ckg/l | 1.0035 | ASTM D4052 |
| Elastomer compatibility, AMS-3217/4 (72hrs @204C), % swell, FTMS 791-3604 | 15.6 | |
| Elastomer compatibility, AMS-3217/1(72hr @70C), % swell, FTMS 791-3604 | 16.4 | |
| Evaporation loss, 6.5 h, 204 C, mass% | 3.0 | ASTM D972(mod) |
| Evaporation loss, 6.5 hr @ 232 C, 29.5" Hg, mass % | 10.9 | ASTM D972(mod) |
| Evaporation loss, 6.5 hr @ 232 C, 5.5" Hg, mass % | 33.7 | ASTM D972(mod) |
| Fire point°C | 285 | ASTM D92 |
| Flash point, Cleveland Open Cup°C | 270 | ASTM D92 |
| Foam, Sequence I, Tendencyml | 8 | ASTM D892 |
| Foam, Sequence II, Tendencyml | 10 | ASTM D892 |
| Foam, Sequence III, Tendencyml | 8 | ASTM D892 |
| Kinematic viscosity @ 100 Cmm2/s | 5.1 | ASTM D445 |
| Kinematic viscosity @ 40 Cmm2/s | 27.6 | ASTM D445 |
| Kinematic viscosity @ -40 Cmm2/s | 11000 | ASTM D445 |
| Pour point°C | -59 | ASTM D5950 |
| Shear stability, %KV loss | 0.9 | ASTM D2603 |
| Total acid number, mgKOH/g, ARP 5088 | 0.03 | |
| Ryder Gear Load carrying, % vs ref., FTMS 791-6508 | 115 |
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